发明名称 THRUST GENERATOR OF FLYING OBJECT
摘要 PROBLEM TO BE SOLVED: To provide a small and light thrust generator of a flying object capable of quickly generating required thrust under a low noise state. SOLUTION: A high pressure gas injection nozzle 13 for injecting high pressure gas is provided on a center axis C of a fan 2. High speed jet from the injection nozzle 13 is surrounded by slip streams of the fan 2, and thereby noise can be reduced. High thrust can be instantaneously generated by the high pressure gas injection, and thereby an attitude control of the flying object can be quickly completed. If the generator is used jointly with a thrust control system by an increase in the number of rotation of the fan 2, only short time injection is required, and thereby small output and reduction in size and weight of the high pressure gas generator are made possible. COPYRIGHT: (C)2006,JPO&NCIPI
申请公布号 JP2006205757(A) 申请公布日期 2006.08.10
申请号 JP20050016661 申请日期 2005.01.25
申请人 TOYOTA MOTOR CORP 发明人 SHINOHARA AKINORI
分类号 B64D27/02;B64B1/36;B64C31/02 主分类号 B64D27/02
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